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Finite Element Analysis (FEA) Implementation of Thermal Barrier Coating (TBC) Lifetime Prediction Methods

机译:热障涂层(TBC)寿命预测方法的有限元分析(FEA)实现

摘要

Thermal Barrier Coatings (TBC) is one of the most important insulation components of an advanced turbine. It is expected to operate at temperature conditions as high as 1760oC. The main objective of this work is to investigate four available methods in predicting the lifespan of the TBC layer and its practicality in finite element analysis (FEA) computation. The four methods discussed are TGO Thickness Calculation, Elasticity and Creep Effect Analysis, A Coupled Oxidation Constitutive Approach and Fracture Mechanics Method. The predicted results obtained are compared with experimental data provided by Limarga [10]. The implementations of TGO Thickness Calculation as well as Elasticity and Creep Effect Analysis in finite element computation have shown a promising result such as local von Mises stress distribution on each layer in TBC (top coat, TGO and bond coat). This simulation result can provide a good comparison data for future experimental work.
机译:隔热涂层(TBC)是先进涡轮机最重要的隔热组件之一。预期可在高达1760oC的温度条件下运行。这项工作的主要目的是研究四种可用的方法来预测TBC层的寿命及其在有限元分析(FEA)计算中的实用性。讨论的四种方法是TGO厚度计算,弹性和蠕变效应分析,氧化本构耦合方法和断裂力学方法。将获得的预测结果与Limarga [10]提供的实验数据进行比较。 TGO厚度计算以及有限元计算中的弹性和蠕变效应分析的实施已显示出令人鼓舞的结果,例如在TBC的每一层(面漆,TGO和粘结涂层)上的局部von Mises应力分布。仿真结果可以为以后的实验工作提供良好的比较数据。

著录项

  • 作者

    Mohamed Hassan;

  • 作者单位
  • 年度 2013
  • 总页数
  • 原文格式 PDF
  • 正文语种 en
  • 中图分类

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